Call Number (LC) Title Results
Y 3.N 21/5:11/L549 Aerodynamic characteristics and flap loads of the brake-flap installation on the 0.40-scale model of the F4F-3 left wing panel / 1
Y 3.N 21/5:11/L55 The effects of static margin and rotational damping in pitch on the longitudinal stability characteristics of an airplane as determined by tests of a model in the NACA free-flight tunnel / 1
Y 3.N 21/5:11/L550 Flight tests of beveled-trailing-edge ailerons with various modifications on a North American XP-51 airplane (AAF No. 41-38) / 1
Y 3.N 21/5:11/L551 XC-35 gust research project preliminary analysis of the lateral distribution of gust velocity along the span of an airplane / 1
Y 3.N 21/5:11/L552 XC-35 gust research project analysis of gust measurements / 1
Y 3.N 21/5:11/L553 Pressure distribution measurements on various surfaces of a 0.2375-scale model of the Douglas XA-26 airplane in the 19-foot pressure tunnel / 1
Y 3.N 21/5:11/L554 XC-35 gust research project characteristics of vertical drafts and associated vertical gust velocities within convective type clouds / 1
Y 3.N 21/5:11/L555 XC-35 gust research project operation in cumulus congestus cloud on July 31, 1941 maximum gust intensities / 1
Y 3.N 21/5:11/L556 Maximum lift coefficients of airplanes based on sum of wing and tail areas / 1
Y 3.N 21/5:11/L557 Data on buckling strength of curved sheet in compression / 1
Y 3.N 21/5:11/L558 On a new method for calculating the potential flow past a body of revolution / 1
Y 3.N 21/5:11/L559 A flight investigation of the stability of a towed body / 1
Y 3.N 21/5:11/L56 WInd-tunnel investigation of a rectangular NACA 2212 airfoil with semispan ailerons and with nonperforated, balanced double split flaps for use as aerodynamic brakes / 1
Y 3.N 21/5:11/L560 Summary of airfoil data / 1
Y 3.N 21/5:11/L561 An investigation of the Ranger V-770-8 engine installation for the Edo XOSE-1 airplane. : 1 - Cooling / 1
Y 3.N 21/5:11/L562 An investigation of the Ranger V-770-8 engine installation for the Edo XOSE-1 airplane. : 2 - Aerodynamics / 1
Y 3.N 21/5:11/L563 Tests of a 0.30 scale semispan model of the Douglas XTB2D-1 airplane wing and fuselage combination in the NACA 19-foot pressure tunnel. : 1 - Full-span flap and air-brake investigation / 1
Y 3.N 21/5:11/L564 Tests of a 0.30-scale semispan model of the Douglas XTB2D-1 airplane wing and fuselage combination in the NACA 19-foot pressure tunnel. : 2 - Roll-flap positioning and lateral-control investigation / 1
Y 3.N 21/5:11/L565 Measurements of the flying qualities of a Hawker Hurricane airplane / 1
Y 3.N 21/5:11/L566 Flying qualities and stalling characteristics of North American XP-51 airplane / 1